TITAN 3C TRANSTAGE DEB, 2789
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 2789 is space debris in LEO originally from a launch on Fri, 15 Oct 1965 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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2789 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TITAN 3C TRANSTAGE DEB
1 2789U 65082KR 25308.60954845 .00420210 00000-0 47080-2 0 9996
2 2789 32.2595 57.3822 0024908 59.9519 300.3624 15.59951238 47245Epoch: 2025-11-04T14:37Z
TLE epoch observation values (Epoch: 2025-11-04T14:37:44.986Z)
Latitude
0.00002°
Longitude
153.85068°
Altitude
377.917 km
Speed
7.69 km/s
True Right ascension
03h 49m 31s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:46:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
408.393 km
Perigee altitude
374.67 km
Semi-major axis
6,769.668 km
Eccentricity
0.00249
Inclination
32.2595°
RAAN
57.3822°
Arg. of periapsis
59.9519°
True anomaly
300.11574°
Mean anomaly
300.3624°
Eccentric anomaly
300.23911°
Mean motion
3.89666 °/min
Orbital period
92.39 mins
BSTAR
0.004708
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Other satellites on launch #82 in the year 1965 (1965-10-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.TITAN 3C TRANSTAGE DEB Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| TITAN 3C TRANSTAGE DEB is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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